1999-041A
M26 was the first of a new group of four launched on 1999 Jul 25. Launch was delayed a day to give STS-93 a third chance to launch.
Mass 448 kg; dispenser is 269 kg. Total stack (4 sats and dispenser) 2061 kg.
| Globalstar 26 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1999 Jul 25 | 0746:03 | Launch by Delta | CC LC17A |
| T+1:03 SRB burnout | |||
| T+1:07 SRB sep | |||
| T+4:24 MECO | |||
| T+4:32 St 1 sep | |||
| T+4:37 St 2 TIG | |||
| T+4:47 PLF sep | |||
| 0757:21 | T+11:18 SECO1 | 185 x 1361 km x 51.9 | |
| 0847:55 | T+1:01:52 SES2 | ||
| 0848:21 | T+1:02:18 SECO2 | 1367 x 1367 km x 52.0 | |
| 0855:13 | T+1:09:10 U1/U2 sep | ||
| 0859:23 | T+1:13:20 L1/L2 sep | ||
| 0934:23 | T+1:48:20 SES3 evasive | ||
| T+1:48:25 SECO3 | 1010 x 1373 x 52 | ||
| 0941:53 | T+1:55:50 SES4 depletion | ||
| T+1:55:56 SECO4 | 422 x 1360 x 52 | ||
| 1999 Jul 25 | 113.13 1369 x 1371 x 52.0 | ||
| 1999 Aug 10 | Orbit raise | ||
| 1999 Aug 12 | 114.08 1412 x 1414 x 52 | ||
| 2010 Sep 7 | 114.08 1413 x 1413 x 52 | ||
| 2010 Sep 10 | Orbit raise | 118.07 1590 x 1597 x 52.0 | |
| 2010 Sep 17 | Orbit raise | 124.24 1866 x 1872 x 52.0 | |
| 2010 Sep 24 | Orbit raise | 127.01 1989 x 1994 x 51.9 | |
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